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contributor authorJaviya, Umesh
contributor authorChew, John
contributor authorHills, Nick
contributor authorDullenkopf, Klaus
contributor authorScanlon, Timothy
date accessioned2017-05-09T00:58:13Z
date available2017-05-09T00:58:13Z
date issued2013
identifier issn1528-8919
identifier othergtp_135_5_051501.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151601
description abstractThe prediction of the preswirl cooling air delivery and disk metal temperature are important for the cooling system performance and the rotor disk thermal stresses and life assessment. In this paper, standalone 3D steady and unsteady computation fluid dynamics (CFD), and coupled FECFD calculations are presented for prediction of these temperatures. CFD results are compared with previous measurements from a direct transfer preswirl test rig. The predicted cooling air temperatures agree well with the measurement, but the nozzle discharge coefficients are under predicted. Results from the coupled FECFD analyses are compared directly with thermocouple temperature measurements and with heat transfer coefficients on the rotor disk previously obtained from a rotor disk heat conduction solution. Considering the modeling limitations, the coupled approach predicted the solid metal temperatures well. Heat transfer coefficients on the rotor disk from CFD show some effect of the temperature variations on the heat transfer coefficients. Reasonable agreement is obtained with values deduced from the previous heat conduction solution.
publisherThe American Society of Mechanical Engineers (ASME)
titleEvaluation of Computational Fluid Dynamics and Coupled Fluid Solid Modeling for a Direct Transfer Preswirl System
typeJournal Paper
journal volume135
journal issue5
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4007752
journal fristpage51501
journal lastpage51501
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 005
contenttypeFulltext


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